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-rw-r--r--src/lib/external_lgpl/tecs/tecs.h6
1 files changed, 3 insertions, 3 deletions
diff --git a/src/lib/external_lgpl/tecs/tecs.h b/src/lib/external_lgpl/tecs/tecs.h
index f8f832ed7..68832a039 100644
--- a/src/lib/external_lgpl/tecs/tecs.h
+++ b/src/lib/external_lgpl/tecs/tecs.h
@@ -71,10 +71,10 @@ public:
// Update of the estimated height and height rate internal state
// Update of the inertial speed rate internal state
// Should be called at 50Hz or greater
- void update_50hz(float baro_altitude, float airspeed, const math::Dcm &rotMat, const math::Vector3 &accel_body, const math::Vector3 &accel_earth);
+ void update_50hz(float baro_altitude, float airspeed, const math::Matrix<3,3> &rotMat, const math::Vector<3> &accel_body, const math::Vector<3> &accel_earth);
// Update the control loop calculations
- void update_pitch_throttle(const math::Dcm &rotMat, float pitch, float baro_altitude, float hgt_dem, float EAS_dem, float indicated_airspeed, float EAS2TAS, bool climbOutDem, float ptchMinCO,
+ void update_pitch_throttle(const math::Matrix<3,3> &rotMat, float pitch, float baro_altitude, float hgt_dem, float EAS_dem, float indicated_airspeed, float EAS2TAS, bool climbOutDem, float ptchMinCO,
float throttle_min, float throttle_max, float throttle_cruise,
float pitch_limit_min, float pitch_limit_max);
// demanded throttle in percentage
@@ -338,7 +338,7 @@ private:
void _update_energies(void);
// Update Demanded Throttle
- void _update_throttle(float throttle_cruise, const math::Dcm &rotMat);
+ void _update_throttle(float throttle_cruise, const math::Matrix<3,3> &rotMat);
// Detect Bad Descent
void _detect_bad_descent(void);